Comparison of calculated and altitude-facility-measured thrust and airflow of two prototype F100 turbofan engines
By: Frank J. Kurtenbach, Dryden Flight Research Center.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; Hugh L. Dryden Flight Research Center.
Series: NASA technical paper ; 1373; NASA technical paper -- 1373.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Informtion Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 26
Subjects: Airplanes -- Turbojet engines.
Notes: Dec. 1978.

Includes bibliographical references.